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Aircraft structures for engineering students /
Aircraft Structures for Engineering Students, Sixth Edition, is the leading self-contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its sixth edition, the author has expanded the book'...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Amsterdam ; Boston :
Butterworth-Heinemann is an imprint of Elsevier,
[2017]
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| Edición: | Sixth edition. |
| Colección: | Elsevier aerospace engineering series.
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| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Part A. Fundamentals of structural analysis. Section A1. Elasticity. Basic elasticity
- Two-dimensional problems in elasticity
- Torsion of solid sections
- Section A2. Virtual work, energy, and matrix methods. Virtual work and energy methods
- Energy methods
- Matrix methods
- Section A3. Thin plate theory. Bending of thin plates
- Section A4. Structural instability. Columns
- Thin plates
- Section A5. Vibration of structures. Structural vibration
- Part B. Analysis of aircraft structures. Section B1. Principles of stressed skin construction. Materials
- Structural components of aircraft
- Section B2. Airworthiness and airframe loads. Airworthiness
- Airframe loads
- Fatigue
- Section B3. Bending, shear and torsion of thin-walled beams. Bending of open and closed, thin-walled beams
- Shear of beams
- Torsion of beams
- Combined open and closed section beams
- Structural idealization
- Section B4. Stress analysis of aircraft components. Wing spars and box beams
- Fuselages
- Wings
- Fuselage frames and wing ribs
- Laminated composite structures
- Section B5. Structural and loading discontinuities. Closed section beams
- Open section beams
- Section B6. Introduction to aeroelasticity. Wing problems
- Appendix : Design of a rear fuselage.